What was found
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. REWORKED AS PER MD-11 CMM 57-44-08. REPAIR EVALUATEDAND FOUND BARREL NUT HOLE MATING SURFACE REMAINING THICKNESS OF UPPER : 0.388" WITHIN REWORK LIMIT AND LOWER : 0.367" BEYOND REWORK LIMIT,MINIMUM THICKNESS= 0.860"- (0.983" / 2) = 0.3685" ACCEPTED AS PER EA # : 1-5750-T0345149 P1 FIGURE 6. TITLE: WINGS-FLIGHT SURFACES- EO 1- 5750-7-5002- RH WING-OUTBD FLAP INBD HINGE ASSY (WING SIDE) -CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.REFER TO EA.# : 1-5750-T0345149 P1 AND SNRM NO. N00587 FOR WORK DETAILS.